GB1249700A - Triple redundant flight control system - Google Patents
Triple redundant flight control systemInfo
- Publication number
- GB1249700A GB1249700A GB46811/69A GB4681169A GB1249700A GB 1249700 A GB1249700 A GB 1249700A GB 46811/69 A GB46811/69 A GB 46811/69A GB 4681169 A GB4681169 A GB 4681169A GB 1249700 A GB1249700 A GB 1249700A
- Authority
- GB
- United Kingdom
- Prior art keywords
- channels
- counter
- expected
- actuate
- rotor
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 title 1
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
- G05D1/0077—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements using redundant signals or controls
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Safety Devices In Control Systems (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Emergency Alarm Devices (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US76424568A | 1968-10-01 | 1968-10-01 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1249700A true GB1249700A (en) | 1971-10-13 |
Family
ID=25070122
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB46811/69A Expired GB1249700A (en) | 1968-10-01 | 1969-09-23 | Triple redundant flight control system |
Country Status (5)
Country | Link |
---|---|
US (1) | US3551776A (de) |
JP (1) | JPS4918399B1 (de) |
DE (1) | DE1949371A1 (de) |
FR (1) | FR2019566A1 (de) |
GB (1) | GB1249700A (de) |
Families Citing this family (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3670148A (en) * | 1970-09-14 | 1972-06-13 | Lear Siegler Inc | Selective signal transmission system |
US3686493A (en) * | 1970-11-13 | 1972-08-22 | Gen Electric | Limited average voter circuitry |
US3827659A (en) * | 1973-03-07 | 1974-08-06 | Bendix Corp | Control system monitoring apparatus having minimal nuisance alarm characteristics |
US3885759A (en) * | 1973-06-21 | 1975-05-27 | Lear Avia Corp | Nose wheel steering system |
GB1481409A (en) * | 1973-10-18 | 1977-07-27 | British Petroleum Co | Monitor systems |
US3881670A (en) * | 1973-12-07 | 1975-05-06 | Bendix Corp | Control system with dual unmonitored condition sensors and fail operative characteristics |
GB1502184A (en) * | 1974-07-05 | 1978-02-22 | Sperry Rand Corp | Automatic flight control systems |
US4105900A (en) * | 1977-02-16 | 1978-08-08 | The Boeing Company | Signal selection apparatus for redundant signal sources |
FR2430633A1 (fr) * | 1978-07-07 | 1980-02-01 | Sfena | Systeme de commande auto-surveille, d'un processus |
US4276648A (en) * | 1979-09-04 | 1981-06-30 | The Boeing Company | Midvalue signal selection and fault detection apparatus and method |
US4472780A (en) * | 1981-09-28 | 1984-09-18 | The Boeing Company | Fly-by-wire lateral control system |
US4472806A (en) * | 1982-05-03 | 1984-09-18 | The Boeing Company | Signal selection and fault detection apparatus |
DE4004086A1 (de) * | 1990-02-10 | 1991-08-14 | Bosch Gmbh Robert | System zur steuerung bzw. regelung einer brennkraftmaschine in einem kraftfahrzeug |
GB2255838A (en) * | 1991-05-13 | 1992-11-18 | Gen Electric | Filtered signal validation. |
JP3206204B2 (ja) * | 1992-05-22 | 2001-09-10 | 株式会社デンソー | スロットルポジションセンサ |
US6462530B1 (en) | 2001-01-25 | 2002-10-08 | Bei Technologies, Inc. | Redundant rate sensor and method |
CN101609329B (zh) * | 2008-06-19 | 2013-04-03 | 北京航空航天大学 | 一种基于单通道双处理器结构的高性能三余度舵机 |
FR3101968B1 (fr) * | 2019-10-14 | 2021-10-08 | Airbus Operations Sas | Système et procédé de commande d’un actionneur d’une gouverne d’un aéronef. |
CN112965467B (zh) * | 2021-02-19 | 2022-03-04 | 四川腾盾科技有限公司 | 一种适用于无人机的三余度信号监控方法 |
CN113296388A (zh) * | 2021-05-27 | 2021-08-24 | 四川腾盾科技有限公司 | 一种三余度无人机舵机输出指令表决方法、系统、计算机程序及存储介质 |
CN113703419B (zh) * | 2021-08-08 | 2024-05-17 | 中国航空工业集团公司沈阳飞机设计研究所 | 一种飞行控制系统余度管理算法的自动测试方法及装置 |
-
1968
- 1968-10-01 US US764245A patent/US3551776A/en not_active Expired - Lifetime
-
1969
- 1969-09-23 GB GB46811/69A patent/GB1249700A/en not_active Expired
- 1969-09-30 DE DE19691949371 patent/DE1949371A1/de active Pending
- 1969-09-30 FR FR6933210A patent/FR2019566A1/fr not_active Withdrawn
- 1969-10-01 JP JP44078066A patent/JPS4918399B1/ja active Pending
Also Published As
Publication number | Publication date |
---|---|
FR2019566A1 (de) | 1970-07-03 |
JPS4918399B1 (de) | 1974-05-09 |
DE1949371A1 (de) | 1970-04-16 |
US3551776A (en) | 1970-12-29 |
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